[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 28th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
362/01:03:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
4
364/11:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2017/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2620792
91 A = 6777268
97 meter
Y = 3347019
01 meter E =
0012309
Z = -5288948
73 I = 51
78090
XDOT = -6535
238933 Wp = 77
68300
YDOT = 3923
216364 meter/sec RA = 153
49367 deg
ZDOT = -754
540346 TA = 185
10775
MA = 185
12032
Ha = 220
014 n
mi
Hp = 215
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8598401
94 X = 2608861
96
Y = 10981033
51 feet Y = 3376260
06 meter
Z = -17352194
01 Z = -5276246
56
XDOT = -21441
072614 XDOT = -6574
958497
YDOT = 12871
444765 feet/sec YDOT = 3849
912803 meter/sec
ZDOT = -2475
526071 ZDOT = -786
382766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10129094
20 X = -3087347
91
Y = 9688064
98 feet Y = 2952922
21 meter
Z = -17296158
46 Z = -5271869
10
XDOT = -14086
119428 XDOT = -4293
449202
YDOT = -19407
070947 feet/sec YDOT = -5915
275225 meter/sec
ZDOT = -2617
688112 ZDOT = -797
871336
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17361
51745382
00016717 00000-0 10270-3 0 9000
2 25544 51
6371 154
5393 0002711 295
2432 64
8439 15
54231253 11819
Satellite: ISS
Catalog Number: 25544
Epoch time: 17361
51745382 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 154
5393 deg
Eccentricity:
0002711
Arg of perigee: 295
2432 deg
Mean anomaly: 64
8439 deg
Mean motion: 15
54231253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 293
Coasting Arc #2 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2017/362/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4018360
82 A = 6778553
36 meter
Y = -2240218
83 meter E =
0003189
Z = 4976550
12 I = 51
80196
XDOT = 5432
468528 Wp = 123
84096
YDOT = -4970
594865 meter/sec RA = 150
80117 deg
ZDOT = 2146
240175 TA = 305
28472
MA = 305
31454
Ha = 220
089 n
mi
Hp = 215
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13183598
49 X = -4017185
09
Y = -7349799
30 feet Y = -2285148
59 meter
Z = 16327264
18 Z = 4957032
89
XDOT = 17823
059474 XDOT = 5477
221917
YDOT = -16307
725934 feet/sec YDOT = -4909
595171 meter/sec
ZDOT = 7041
470390 ZDOT = 2172
737864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1912403
51 X = -582900
59
Y = 15066079
12 feet Y = 4592140
92 meter
Z = 16240761
89 Z = 4950184
23
XDOT = -20626
293214 XDOT = -6286
894172
YDOT = -10346
122168 feet/sec YDOT = -3153
498037 meter/sec
ZDOT = 7160
015054 ZDOT = 2182
372588
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17362
09613597
00016717 00000-0 10270-3 0 9017
2 25544 51
6377 151
6573 0003170 301
7383 58
3460 15
54256613 11900
Satellite: ISS
Catalog Number: 25544
Epoch time: 17362
09613597 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 151
6573 deg
Eccentricity:
0003170
Arg of perigee: 301
7383 deg
Mean anomaly: 58
3460 deg
Mean motion: 15
54256613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 301
Coasting Arc #3 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2017/363/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2547882
51 A = 6777103
24 meter
Y = 3336246
99 meter E =
0012608
Z = -5331170
31 I = 51
82523
XDOT = -6241
535222 Wp = 79
14992
YDOT = 4435
134533 meter/sec RA = 145
81243 deg
ZDOT = -205
557632 TA = 188
88259
MA = 188
90492
Ha = 220
163 n
mi
Hp = 215
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8359194
58 X = 2536282
59
Y = 10945692
24 feet Y = 3364674
68 meter
Z = -17490716
25 Z = -5318821
40
XDOT = -20477
477763 XDOT = -6289
667705
YDOT = 14550
966317 feet/sec YDOT = 4365
068306 meter/sec
ZDOT = -674
401680 ZDOT = -235
993728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6828427
27 X = 2081304
63
Y = -12039905
37 feet Y = -3669763
16 meter
Z = -17436247
51 Z = -5314568
24
XDOT = 20443
864912 XDOT = 6231
290025
YDOT = 12777
430890 feet/sec YDOT = 3894
560935 meter/sec
ZDOT = -810
412936 ZDOT = -247
013863
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17363
06060676
00016717 00000-0 10270-3 0 9020
2 25544 51
6380 146
8476 0003154 308
5111 51
5759 15
54222536 12058
Satellite: ISS
Catalog Number: 25544
Epoch time: 17363
06060676 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 146
8476 deg
Eccentricity:
0003154
Arg of perigee: 308
5111 deg
Mean anomaly: 51
5759 deg
Mean motion: 15
54222536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 292
Coasting Arc #4 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2017/364/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -989710
27 A = 6778049
31 meter
Y = -4356859
65 meter E =
0005560
Z = 5096663
90 I = 51
85497
XDOT = 6560
214123 Wp = 21
73215
YDOT = -3559
247995 meter/sec RA = 140
82646 deg
ZDOT = -1763
042078 TA = 85
29636
MA = 85
23287
Ha = 220
285 n
mi
Hp = 215
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3247080
95 X = -965674
27
Y = -14294158
96 feet Y = -4367793
35 meter
Z = 16721338
26 Z = 5091914
16
XDOT = 21523
012215 XDOT = 6608
091029
YDOT = -11677
322818 feet/sec YDOT = -3485
619333 meter/sec
ZDOT = -5784
258785 ZDOT = -1731
058582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11741777
31 X = -3578893
72
Y = 8813790
82 feet Y = 2686443
44 meter
Z = 16700821
09 Z = 5090410
27
XDOT = -18709
928577 XDOT = -5702
786230
YDOT = -14200
561897 feet/sec YDOT = -4328
331266 meter/sec
ZDOT = -5641
461238 ZDOT = -1719
517385
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17364
08937185
00016717 00000-0 10270-3 0 9032
2 25544 51
6379 141
7189 0003151 314
2536 45
8358 15
54225335 12212
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
08937185 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 141
7189 deg
Eccentricity:
0003151
Arg of perigee: 314
2536 deg
Mean anomaly: 45
8358 deg
Mean motion: 15
54225335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 308
Coasting Arc #5 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3509241
90 A = 6777319
56 meter
Y = -2420747
51 meter E =
0000726
Z = 5267905
86 I = 51
86349
XDOT = 5210
983605 Wp = 96
46855
YDOT = -5551
706188 meter/sec RA = 138
63014 deg
ZDOT = 919
973097 TA = 344
75825
MA = 344
76044
Ha = 220
264 n
mi
Hp = 215
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11513260
82 X = -3507500
55
Y = -7942085
01 feet Y = -2459981
06 meter
Z = 17283155
69 Z = 5250863
01
XDOT = 17096
402904 XDOT = 5268
208205
YDOT = -18214
259148 feet/sec YDOT = -5493
113539 meter/sec
ZDOT = 3018
284439 ZDOT = 945
424875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7006210
27 X = 2135492
89
Y = -12212635
21 feet Y = -3722411
21 meter
Z = 17207670
34 Z = 5244897
92
XDOT = 18604
129280 XDOT = 5670
538605
YDOT = 15087
239549 feet/sec YDOT = 4598
590615 meter/sec
ZDOT = 3132
314772 ZDOT = 954
729543
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17364
53945531
00016717 00000-0 10270-3 0 9047
2 25544 51
6375 139
4704 0002882 307
9591 52
1301 15
54241796 12280
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
53945531 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 139
4704 deg
Eccentricity:
0002882
Arg of perigee: 307
9591 deg
Mean anomaly: 52
1301 deg
Mean motion: 15
54241796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 311
Coasting Arc #6 (Orbit 1242)
---------------------------------------
Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2158956
49 A = 6777334
18 meter
Y = 3709435
66 meter E =
0012099
Z = -5255564
24 I = 51
88899
XDOT = -5806
858133 Wp = 90
68068
YDOT = 4881
247777 meter/sec RA = 133
64625 deg
ZDOT = 1061
781980 TA = 189
45488
MA = 189
47768
Ha = 220
222 n
mi
Hp = 215
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7083190
60 X = 2142844
99
Y = 12170064
49 feet Y = 3733489
15 meter
Z = -17242664
83 Z = -5245115
41
XDOT = -19051
371827 XDOT = -5866
167579
YDOT = 16014
592443 feet/sec YDOT = 4815
979768 meter/sec
ZDOT = 3483
536680 ZDOT = 1033
430701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11426473
12 X = -3482789
01
Y = 8324706
62 feet Y = 2537370
58 meter
Z = -17196700
87 Z = -5241554
43
XDOT = -17154
585399 XDOT = -5228
717630
YDOT = -16625
695080 feet/sec YDOT = -5067
511860 meter/sec
ZDOT = 3356
673218 ZDOT = 1023
113997
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17365
50391832
00016717 00000-0 10270-3 0 9055
2 25544 51
6388 134
6625 0002824 312
0208 48
0704 15
54254678 12432
Satellite: ISS
Catalog Number: 25544
Epoch time: 17365
50391832 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 134
6625 deg
Eccentricity:
0002824
Arg of perigee: 312
0208 deg
Mean anomaly: 48
0704 deg
Mean motion: 15
54254678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1243
Checksum: 301
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